In sonic and supersonic flows, Mach waves are formed. The local Mach wave angle is called a Mach angle μ, and it is related to the local Mach number via
Each Mach wave causes an infinitesimal turn of the flow and a corresponding infinitesimal change in fluid pressure, temperature, density, and Mach number. Through infinitely many such waves, that is, Mach waves, flow can turn a finite angle and attain a finite change in static pressure, static temperature, static density, and Mach number. The Prandtl–Meyer function defines an angle (in radians) that a sonic flow has to turn in order to achieve a supersonic Mach number M.
A graphical representation of the Prandtl–Meyer function and the Mach angle is shown.
M | v (deg) | (deg) | M | v (deg) | (deg) | M | v (deg) | (deg) |
1.0 | 0.00 | 90.00 | 5.4 | 80.43 | 10.67 | 28 | 120.2 | 2.05 |
1.1 | 1.34 | 65.38 | 5.5 | 81.25 | 10.48 | 29 | 120.6 | 1.98 |
1.2 | 3.56 | 56.44 | 5.6 | 82.03 | 10.29 | 30 | 120.9 | 1.91 |
1.3 | 6.17 | 50.28 | 5.7 | 82.80 | 10.10 | 31 | 121.2 | 1.85 |
1.4 | 8.99 | 45.58 | 5.8 | 83.54 | 9.93 | 32 | 121.5 | 1.79 |
1.5 | 11.91 | 41.81 | 5.9 | 84.26 | 9.76 | 33 | 121.8 | 1.74 |
1.6 | 14.86 | 38.68 | 6 | 84.96 | 9.59 | 34 | 122.0 | 1.69 |
1.7 | 17.81 | 36.03 | 6.2 | 86.30 | 9.28 | 35 | 122.3 | 1.64 |
1.8 | 20.73 | 33.75 | 6.4 | 87.56 | 8.99 | 36 | 122.5 | 1.59 |
1.9 | 23.59 | 31.76 | 6.6 | 88.76 | 8.71 | 37 | 122.7 | 1.55 |
2.0 | 26.38 | 30.00 | 6.8 | 89.90 | 8.46 | 38 | 122.9 | 1.51 |
2.1 | 29.10 | 28.44 | 7 | 90.97 | 8.21 | 39 | 123.1 | 1.47 |
2.2 | 31.73 | 27.04 | 7.5 | 93.44 | 7.66 | 40 | 123.3 | 1.43 |
2.3 | 34.28 | 25.77 | 8 | 95.63 | 7.18 | 50 | 124.7 | 1.15 |
2.4 | 36.75 | 24.62 | 8.5 | 97.57 | 6.76 | 60 | 125.7 | 0.95 |
2.5 | 39.12 | 23.58 | 9 | 99.32 | 6.38 | 70 | 126.4 | 0.82 |
2.6 | 41.42 | 22.62 | 9.5 | 100.89 | 6.04 | 80 | 126.9 | 0.72 |
2.7 | 43.62 | 21.74 | 10 | 102.32 | 5.74 | 90 | 127.3 | 0.64 |
2.8 | 45.75 | 20.92 | 10.5 | 103.61 | 5.47 | 100 | 127.6 | 0.57 |
2.9 | 47.79 | 20.17 | 11 | 104.80 | 5.22 | |||
3.0 | 49.76 | 19.47 | 11.5 | 105.88 | 4.99 | |||
3.1 | 51.65 | 18.82 | 12 | 106.88 | 4.78 | |||
3.2 | 53.47 | 18.21 | 12.5 | 107.80 | 4.59 | |||
3.3 | 55.22 | 17.64 | 13 | 108.65 | 4.41 | |||
3.4 | 56.91 | 17.10 | 13.5 | 109.44 | 4.25 | |||
3.5 | 58.53 | 16.60 | 14 | 110.18 | 4.10 | |||
3.6 | 60.09 | 16.13 | 14.5 | 110.87 | 3.95 | |||
3.7 | 61.60 | 15.68 | 15 | 111.51 | 3.82 | |||
3.8 | 63.05 | 15.26 | 15.5 | 112.11 | 3.70 | |||
3.9 | 64.44 | 14.86 | 16 | 112.68 | 3.58 | |||
4.0 | 65.79 | 14.48 | 16.5 | 113.21 | 3.47 | |||
4.1 | 67.08 | 14.12 | 17 | 113.71 | 3.37 | |||
4.2 | 68.33 | 13.77 | 17.5 | 114.18 | 3.28 | |||
4.3 | 69.54 | 13.45 | 18 | 114.63 | 3.18 | |||
4.4 | 70.71 | 13.14 | 18.5 | 115.05 | 3.10 | |||
4.5 | 71.83 | 12.84 | 19 | 115.45 | 3.02 | |||
4.6 | 72.92 | 12.56 | 20 | 116.2 | 2.87 | |||
4.7 | 73.97 | 12.28 | 21 | 116.9 | 2.73 | |||
4.8 | 74.99 | 12.02 | 22 | 117.5 | 2.61 | |||
4.9 | 75.97 | 11.78 | 23 | 118.0 | 2.49 | |||
5 | 76.92 | 11.54 | 24 | 118.6 | 2.39 | |||
5.1 | 77.84 | 11.31 | 25 | 119.0 | 2.29 | |||
5.2 | 78.73 | 11.09 | 26 | 119.5 | 2.20 | |||
5.3 | 79.60 | 10.88 | 27 | 119.9 | 2.12 |
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